View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 27386U 02009A 23263.92470260 .00000248 00000-0 95090-4 0 9994
2 27386 98.2419 230.0451 0001217 86.9062 292.2283 14.38408229129728
| Epoch (UTC): | 20 September 2023 22:11:34 |
| Eccentricity: | 0.0001217 |
| inclination: | 98.2419° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 230.0451° |
| argument of perigee: | 86.9062° |
| revolutions per day: | 14.38408229 |
| mean anomaly at epoch: | 292.2283° |
| orbit number at epoch: | 12972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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